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US2265737A - Fluid control apparatus - Google Patents

Fluid control apparatus Download PDF

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Publication number
US2265737A
US2265737A US280322A US28032239A US2265737A US 2265737 A US2265737 A US 2265737A US 280322 A US280322 A US 280322A US 28032239 A US28032239 A US 28032239A US 2265737 A US2265737 A US 2265737A
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US
United States
Prior art keywords
fluid
flow
duct
orifice
inlet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US280322A
Inventor
Kenton D Mcmahan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US280322A priority Critical patent/US2265737A/en
Application granted granted Critical
Publication of US2265737A publication Critical patent/US2265737A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K13/00Other constructional types of cut-off apparatus; Arrangements for cutting-off
    • F16K13/08Arrangements for cutting-off not used
    • F16K13/10Arrangements for cutting-off not used by means of liquid or granular medium
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/206Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/218Means to regulate or vary operation of device
    • Y10T137/2202By movable element
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/206Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/2273Device including linearly-aligned power stream emitter and power stream collector
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/87571Multiple inlet with single outlet

Definitions

  • the present invention relates to fluid control apparatus by means of which the main flow of fluid in a duct is controlled by means of a relatively small secondary fluid flow.
  • the object of my invention is to provide an improved construction and arrangement in fluid flow apparatus of this type, and for a consideration of what I believe novel and my invention,
  • Fig. 1 is a sectional view of fluid flow apparatus embodying my invention
  • Fig. 2 is a curve showing the variation in the main fluid flow in accordance with variations in the pressure of the secondary fluid flow.
  • a duct orcasing l which is supplied by a fan 2 located at the inlet 3.
  • the fan is driven by an electric motor 4 connected to'line conductors 5 and 6 in one of which is located a control switch I.
  • the switch 1 When the switch 1 is closed the fan is rotated to supply fluid to the duct I.
  • the fluid discharged from the fan flows axially along the duct 1 through an orifice 8 having outwardly flaring curved walls 9 provided at their outer edges with a flange l8 fixed to the inner surface of the duct.
  • the Walls 9 decrease the loss in the fluid flowing through the orifice 8.
  • the orifice 8 is concentric with and in closely spaced proximity to the inlet orifice l l of a reentrant diffuser duct 12 which is supported in the duct I by a flange I3 at its outlet fixed to the inner surface of the duct.
  • the orifice 8 and the inlet II are of substantially the same size and in axial alignment so that the fluid discharge of the orifice 8 is directed into the difiuser along its axis without change of direction.
  • the inlet H is preferably a sharp edged orifice.
  • the walls of the duct 1 between the flanges l and I3 enclose the space around the'orifice 8 and inlet II.
  • This space is supplied with a secondary fluid stream conducted thereto by a conduit l4 supplied by a fan 15 driven by an electric motor IS.
  • the armature of the motor is connected across line conductors and 6 by conductors l1 and 18.
  • a variable resistance I9 is connected in the conductor l8.
  • the field 20 of the motor I8 is connected by conductors 2
  • the switch is connected to contacts 25 and 26 the reverse direction and the motor accordingly rotates in the reverse direction.
  • the amount and direction of the secondary fluid flow through the duct 14 may be varied.
  • the secondary fluid flow in the region of the orifices 8 and H may be radially inward or outward through the space between the orifices, in other words, in a direction transverse to the direction of the main flow. It has been observed experimentally that the flow of the main fluid stream from the fan, 2, designated as Ql, is a minimum when the flow and pressure of the secondary fluid stream, designated respectively as Q2 and H2, are a maximum. As the secondary flow and pressure decrease to zero, the main flow increases. The main flow continues to increase as the secondary flow and head become negative, or, in other words, are. changed from pressure to suction.
  • the present construcftion a large change in the main flow Qi is effected by a. relatively small change in the secondary fluid pressure or potential H2.
  • the fan I5 which supplies the secondary fluid flow, has a capacity equal to about 10% of the fan 2 which supplied the main fluid flow.
  • the variation in main flow is due to changes in the effective orifice coefficient of the diffuser inlet II and to changes in the resistance of the diffuser duct 12.
  • the 5 fluid from the orifice 8 should flow straight across the space between the orifice and the difiuser inlet II, and from there should flow parallel to the inner walls of the diffuser duct without eddying.
  • this flow condition is obtained when a suction is applied to the duct H, which causes the fluid to flow along the paths indicated by the arrows in Fig. 1 in the lower half of the diffuser.
  • the minimum main flow is obtained when the duct I4 is subfield is connected across the line conductors in jected to its maximum pressure, causing the 2 acorns? greatest secondary fiow to the space around the difiuser duct and the orifices 3 and H.
  • the fluid flow conditions present at this time are illusaccordingly decreases. The extreme conditions,
  • the sharpness of the control afforded by varye ing the secondary air flow is dependent upon the spacing of the orifices 8 and H and the inclination of the diffusion duct 32.
  • the orifices a and i i should be closely spaced and the difiuser duct should have a relatively small angle of inclination.
  • the inlet opening ii of the difiuser duct be a sharp edged orifice since this type of orifice is subject to the greatest change in resistance under the conditions present.
  • Fluid fiow apparatus for controlling the flow of a fluid stream.
  • a duct having an inlet, adischarge orifice for said fluid stream arranged to discharge said stream along the axis of the duct, the inlet of said duct being in closely spaced prom'mity to the discharge orifice, a casing enclosing the space around and between the discharge orifice and said inlet, and means for introducing a controlling fluid stream of the same fluid as the said fluid stream into said casing, said means including means for varying the pressure in said casing between positive and negative values to control the flow through the orifice.
  • Fluid flow apparatus for controlling the flow of a fluid stream, comprising a discharge orifice for said fluid stream, an aligned difi'user duct for receiving said stream having an entrance orifice in closely spaced proximity to said discharge orifice, a casingenclosing the space between said orifices, provisions for conducting a controlling fluid stream of-the same fluid as the said fluid stream to said casing transverse to the said fluid stream, and means for varying the pressure of the controlling stream between positive and negative values to control the flow of the main stream.
  • Fluid flow apparatus comprising a casing, a
  • duct having an inlet orifice in the casing, means for efi'ecting'a main fluid flow into said duct having a discharge orifice in the casing closely spaced from the inlet orifice and arranged to discharge substantially all of its flow axially into said inlet oriflce, the arrangement'of said means and duct effecting a pressure in said casing above absolute zero pressure, and means independent of said first means for increasing or decreasing the pressure within the casing for controlling the fiow effected by said first means.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Jet Pumps And Other Pumps (AREA)

Description

Dec. 9, 1941. K. D. M MAHAN FLUID CONTROL APPARATUS Filed June 21, 1939 Fig. I
-Fig.2.
Inventor: Kenton D. McMahan,
His Attorney.
Patented Dee. 9, 1941 FLUID CONTROL APPARATUS Kenton D. McMahan, Scotia, N. Y., assignor to General Electric New York Company, a corporation of Application June 21, 1939, Serial No. 280,322
3 Claims.
The present invention relates to fluid control apparatus by means of which the main flow of fluid in a duct is controlled by means of a relatively small secondary fluid flow.
The object of my invention is to provide an improved construction and arrangement in fluid flow apparatus of this type, and for a consideration of what I believe novel and my invention,
attention is directed to the following description and the claims appended thereto.
In the accompanying drawing, Fig. 1 is a sectional view of fluid flow apparatus embodying my invention, and Fig. 2 is a curve showing the variation in the main fluid flow in accordance with variations in the pressure of the secondary fluid flow.
Referring to the drawing; there is shown a duct orcasing lwhich is supplied by a fan 2 located at the inlet 3. The fan is driven by an electric motor 4 connected to'line conductors 5 and 6 in one of which is located a control switch I. When the switch 1 is closed the fan is rotated to supply fluid to the duct I. The fluid discharged from the fan flows axially along the duct 1 through an orifice 8 having outwardly flaring curved walls 9 provided at their outer edges with a flange l8 fixed to the inner surface of the duct. The Walls 9 decrease the loss in the fluid flowing through the orifice 8. The orifice 8 is concentric with and in closely spaced proximity to the inlet orifice l l of a reentrant diffuser duct 12 which is supported in the duct I by a flange I3 at its outlet fixed to the inner surface of the duct. The orifice 8 and the inlet II are of substantially the same size and in axial alignment so that the fluid discharge of the orifice 8 is directed into the difiuser along its axis without change of direction. The inlet H is preferably a sharp edged orifice. The walls of the duct 1 between the flanges l and I3 enclose the space around the'orifice 8 and inlet II. This space is supplied with a secondary fluid stream conducted thereto by a conduit l4 supplied by a fan 15 driven by an electric motor IS. The armature of the motor is connected across line conductors and 6 by conductors l1 and 18. A variable resistance I9 is connected in the conductor l8. The field 20 of the motor I8 is connected by conductors 2| and 22 to a reversing switch 23 providedwith contacts 24, 25, and 26, When the switch is connected to contacts 24 and 25 the field is connected across line conductors 5 and 6 through conductors 21 and 28. When the switch is connected to contacts 25 and 26 the the reverse direction and the motor accordingly rotates in the reverse direction. By varying the position of the switch 23 and the resistance of the variable resistance I9, the amount and direction of the secondary fluid flow through the duct 14 may be varied. The secondary fluid flow in the region of the orifices 8 and H may be radially inward or outward through the space between the orifices, in other words, in a direction transverse to the direction of the main flow. It has been observed experimentally that the flow of the main fluid stream from the fan, 2, designated as Ql, is a minimum when the flow and pressure of the secondary fluid stream, designated respectively as Q2 and H2, are a maximum. As the secondary flow and pressure decrease to zero, the main flow increases. The main flow continues to increase as the secondary flow and head become negative, or, in other words, are. changed from pressure to suction. The increase in main flow continues until the maximum capacity of the difluser duct I2 is reached. Theq'changes in the main flow are shown diagrammatically in Fig. 2. As can be seen from thisburve, the main flow varies in a manner similar to the plate current in a grid controlled vacuum tube. In the vacuum tube a large change in plate'current is effected by a relatively small change in the grid potential. In
the present construcftion a large change in the main flow Qi is effected by a. relatively small change in the secondary fluid pressure or potential H2. In the construction illustrated the fan I5, which supplies the secondary fluid flow, has a capacity equal to about 10% of the fan 2 which supplied the main fluid flow. By changing the secondary fluid flow it is possible to effect a variation of ten or more to one in the main fluid flow. This variation is effected without the use of dampers.
The variation in main flow is due to changes in the effective orifice coefficient of the diffuser inlet II and to changes in the resistance of the diffuser duct 12. For minimum resistance the 5 fluid from the orifice 8 should flow straight across the space between the orifice and the difiuser inlet II, and from there should flow parallel to the inner walls of the diffuser duct without eddying. In the present construction this flow condition is obtained when a suction is applied to the duct H, which causes the fluid to flow along the paths indicated by the arrows in Fig. 1 in the lower half of the diffuser. The minimum main flow is obtained when the duct I4 is subfield is connected across the line conductors in jected to its maximum pressure, causing the 2 acorns? greatest secondary fiow to the space around the difiuser duct and the orifices 3 and H. The fluid flow conditions present at this time are illusaccordingly decreases. The extreme conditions,
have been explained above. In the intermediate conditions the fluid fiow conditions are in between the conditions illustrated.
The sharpness of the control afforded by varye ing the secondary air flow is dependent upon the spacing of the orifices 8 and H and the inclination of the diffusion duct 32. For best results the orifices a and i i should be closely spaced and the difiuser duct should have a relatively small angle of inclination. It is also preferable that the inlet opening ii of the difiuser duct be a sharp edged orifice since this type of orifice is subject to the greatest change in resistance under the conditions present.
The position of the zero axis in Fig.2, i. e., the position corresponding to zero secondary head H2, varies with the relative diameters of the orifices 8 and: ii. If the orificefi is larger than the orifice H, the zero axis will be shifted to the right in Fig. 2. That is, there will be a greater main fiow when the secondary head is zero. If the orifice 8 is smaller than the orifice H, the zero axis will be shifted to the left. 'A
3 greater negative secondary head will then be required to produce the maximum main flow.
. What I claim as new and desire to secure by Letters Patent of the United States is:
1. Fluid fiow apparatus for controlling the flow of a fluid stream. comprising a duct having an inlet, adischarge orifice for said fluid stream arranged to discharge said stream along the axis of the duct, the inlet of said duct being in closely spaced prom'mity to the discharge orifice, a casing enclosing the space around and between the discharge orifice and said inlet, and means for introducing a controlling fluid stream of the same fluid as the said fluid stream into said casing, said means including means for varying the pressure in said casing between positive and negative values to control the flow through the orifice.
2. Fluid flow apparatus for controlling the flow of a fluid stream, comprising a discharge orifice for said fluid stream, an aligned difi'user duct for receiving said stream having an entrance orifice in closely spaced proximity to said discharge orifice, a casingenclosing the space between said orifices, provisions for conducting a controlling fluid stream of-the same fluid as the said fluid stream to said casing transverse to the said fluid stream, and means for varying the pressure of the controlling stream between positive and negative values to control the flow of the main stream.
3. Fluid flow apparatus comprising a casing, a
' duct having an inlet orifice in the casing, means for efi'ecting'a main fluid flow into said duct having a discharge orifice in the casing closely spaced from the inlet orifice and arranged to discharge substantially all of its flow axially into said inlet oriflce, the arrangement'of said means and duct effecting a pressure in said casing above absolute zero pressure, and means independent of said first means for increasing or decreasing the pressure within the casing for controlling the fiow effected by said first means.
KENTON D. MCMAHAN.
US280322A 1939-06-21 1939-06-21 Fluid control apparatus Expired - Lifetime US2265737A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421877A (en) * 1945-08-27 1947-06-10 Rohr Aircraft Corp Suction attachment
US3305170A (en) * 1964-04-01 1967-02-21 Sperry Rand Corp Pure fluid operated counter
US3425433A (en) * 1966-04-20 1969-02-04 Moore Products Co Flow control valve
US3474813A (en) * 1963-12-07 1969-10-28 Snecma Flow control device for multi-conduit structures
US3665949A (en) * 1969-06-27 1972-05-30 Bendix Corp Gaseous controlled fluidic throttling valve
US4446695A (en) * 1979-10-03 1984-05-08 Burtis Wilson A Aircraft propulsion assembly
US6000418A (en) * 1997-03-20 1999-12-14 International Business Machines Corporation Integrated dynamic fluid mixing apparatus and method

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421877A (en) * 1945-08-27 1947-06-10 Rohr Aircraft Corp Suction attachment
US3474813A (en) * 1963-12-07 1969-10-28 Snecma Flow control device for multi-conduit structures
US3305170A (en) * 1964-04-01 1967-02-21 Sperry Rand Corp Pure fluid operated counter
US3425433A (en) * 1966-04-20 1969-02-04 Moore Products Co Flow control valve
US3665949A (en) * 1969-06-27 1972-05-30 Bendix Corp Gaseous controlled fluidic throttling valve
US4446695A (en) * 1979-10-03 1984-05-08 Burtis Wilson A Aircraft propulsion assembly
US6000418A (en) * 1997-03-20 1999-12-14 International Business Machines Corporation Integrated dynamic fluid mixing apparatus and method

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